# Service difficulty reports: N997AT

A list on [N997AT](https://openairdocs.org/aircraft/N997AT.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 5 · 206 reports

- [SDR DALA2026090705016](https://openairdocs.org/sdr/DALA2026090705016.md): Latch · detached · Sep 4, 2026 · N997AT · Boeing 717200 · Emergency Equipment
  > GIRT BAR CAME OFF AND CAME UNLATCHED. REATTACHED L1 DOOR GIRT BAR LATCH PER AMM 25-61. (7631672) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026021901200](https://openairdocs.org/sdr/DALA2026021901200.md): Skin · cracked · Feb 15, 2026 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > AIRCRAFT 9545, CRACK ON UPPER FUSELAGE SKIN STA Y=1152 BTW LONG 2L & 3L AFT FUSELAGE. CORRECTIVE ACTION: CRACK ON UPPER FUSELAGE SKIN STA Y=1152 BTW LONG 2L & 3L AFT FUSELAGE WAS REPAIRED PER PRI 632025-14 REV. 4 AND ER/A 632025-14. (LP 1452829)
- [SDR DALA2026021901197](https://openairdocs.org/sdr/DALA2026021901197.md): Hinge Fitting · excess play · Feb 15, 2026 · N997AT · Boeing 717200 · Trailing Edge Flaps
  > AFTER REMOVING SEALANT, FOUND FREE PLAY ON FLAP HINGE NR 3 AT RT WING. FLAP HINGE NR 3 AT RT WING WAS REPAIRED IAW PRI 632047-14, REV 3, & ER/A 632047-14, REV ORIGINAL. (LP 1452662)
- [SDR DALA2026021801118](https://openairdocs.org/sdr/DALA2026021801118.md): Doubler · cracked · Feb 12, 2026 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED DOUBLER, BS 1178, BTW LONGERONS 15 -16L, AFT ACCESSORY COMPARMENT. REPAIRED IAW PRI 632147-14 (1448393).
- [SDR DALA2026021801113](https://openairdocs.org/sdr/DALA2026021801113.md): Skin · cracked · Feb 9, 2026 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACKED EXTERNAL FUSELAGE SKIN BS 1087 BTW LONGERONS 12 - 13R. REPAIRED IAW PRI 631947-14 (1442449).
- [SDR DALA2026020900906](https://openairdocs.org/sdr/DALA2026020900906.md): Lanyard · damaged · Feb 3, 2026 · N997AT · Boeing 717200 · Emergency Equipment
  > BROKEN THREADS LANYARD ON RT & LT DOOR SLIDE DEPLOYMENT AT CPAX. REPAIRED PER AMDS 5211-4002 (1434470)
- [SDR DALA2026020900913](https://openairdocs.org/sdr/DALA2026020900913.md): Skin · cracked · Feb 2, 2026 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, BS 1087, L13L TO L14L, CRACKED. REPAIRED IAW ERA 631962-14. (1439311)
- [SDR DALA2026020900912](https://openairdocs.org/sdr/DALA2026020900912.md): Skin · cracked · Feb 2, 2026 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN, Y=1087, L13R TO L14R CRACKED. REPAIRED IAW ER/A 631947-14. (1435871)
- [SDR DALA2025120108774](https://openairdocs.org/sdr/DALA2025120108774.md): Oil System · leaking · Nov 27, 2025 · N997AT · Boeing 717200 · APU Oil System
  > SHIP 9545 MUSTY SOCK SMELL FROM FORWARD GALLEY VENT. FOUND APU OIL LEAKING. R/R APU PER B717 AMM 49-10 OPS CHK GOOD (7952228)
- [SDR DALA2025112308529](https://openairdocs.org/sdr/DALA2025112308529.md): Sign · dislodged · Nov 21, 2025 · N997AT · Boeing 717200 · Emergency Lighting
  > FWD EXIT SIGN DAMAGED. (F/A REPORTED PASSENGER HIT IT WITH HIS BAG). RESECURED, OPS NORMAL. (LP 7952210)
- [SDR DALA2025102407797](https://openairdocs.org/sdr/DALA2025102407797.md): Warning Message · false activation · Oct 21, 2025 · N997AT · Boeing 717200 · Stabilizer Control System
  > ATO- DURING TAKEOFF ROLL THE CREW REPORTED A STAB OUT OF TRIM AURAL WARNING AND ABORTED TAKEOFF. MAINTENANCE PERFORMED STABILIZER SYSTEM TESTS AND RETURNED TO SERVICE.(7843690)
- [SDR DALA2024112711260](https://openairdocs.org/sdr/DALA2024112711260.md): Fastener · loose · Nov 24, 2024 · N997AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- FOUND LOOSE FASTENERS ON RH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY NRC 018-0001:5530-01048-02 / 002 00005: CHECK IF THE FASTENER(S) HOLE COUNTER SINK AND DIAMETER ARE WITHIN LIMITS LISTED IN SERVICE GENERAL DRAWING SG
- [SDR DALA2024112611225](https://openairdocs.org/sdr/DALA2024112611225.md): Fastener · loose · Nov 24, 2024 · N997AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > -AD- FOUND LOOSE FASTENERS ON LH VERTICAL STABILIZER LEADING EDGE REF AA 553001048 AND AD 2018-10-08. SUMMARY OF NRC 018-0001:5530-01048-02 /001 00004: CHECKED AND FOUND OK. SUMMARY OF NRC 018-0001:5530-01048-02/001 00004: CMOR VERIFIED LH FASTENER HOLES LIMIT
- [SDR DALA2024020601580](https://openairdocs.org/sdr/DALA2024020601580.md): Skin · bent · Feb 6, 2024 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > BENT ON EDGE EXTERNAL SKIN AFT UPPER, AFT LOWER, AND BEAM #4 AT SERVICE DOOR L1. SUMMARY OF NRC 00069: EXTERNAL SKIN ON AFT UPPER EDGE AND EDGE OF EXTERNAL SKIN AT BEAM #4 WAS CONFORMED PER B717 SRM-51-20-09-0G. AFT LOWER EDGE OF EXTERNAL SKIN AT SERVICE DOOR
- [SDR DALA2024020301512](https://openairdocs.org/sdr/DALA2024020301512.md): Web · cracked · Feb 2, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK MEMBRANE ON UPPER SURFACE OF CENTER WING STA Y=715 AND -X=44 UNDER RH MIDDLE SEAT TRACK AT WING BOX AREA. SUMMARY OF NRC 00357: MEMBRANE ON UPPER SURFACE OF CENTER WING STA Y=715 AND -X=44 UNDER RH MIDDLE SEAT TRACK AT WING BOX AREA WAS REPAIRED PER PRI
- [SDR DALA2024020301508](https://openairdocs.org/sdr/DALA2024020301508.md): Skin · corroded · Feb 1, 2024 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CORROSION ON INNER SKIN BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT (C1). SUMMARY OF NRC 00166: CORROSION LEVEL 2. INTERNAL SKIN DOUBLER BTW STA Y=655/663 AND BTW LONGERONS 29L/29R AT FWD CARGO COMPARTMENT WAS REPAIRED PER ERA 614961-1
- [SDR DALA2024020301506](https://openairdocs.org/sdr/DALA2024020301506.md): Door Frame · corroded · Feb 1, 2024 · N997AT · Boeing 717200 · Fuselage Main, Structure
  > CORROSION ON DOOR JAMB STA 951 TO STA 994 AT AFT CARGO COMPARTMENT. C2. SUMMARY OF NRC 00071: CORROSION LEVEL 2. PREVIOUS REPAIR SECTION OF DOOR JAMB STA 951 TO STA 994 AT AFT CARGO COMPARTMENT WAS REPLACED PER B717-200 SRM 53-20-15-2R PROCEDURE 7 REPAIR 7. (L
- [SDR DALA2024020101448](https://openairdocs.org/sdr/DALA2024020101448.md): Longeron · corroded · Feb 1, 2024 · N997AT · Boeing 717200 · Fuselage Main, Longeron/Stringer
  > CORROSION ON LOWER SURFACE LONGERON END STA 360 L26R AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00172: CORROSION LEVEL 2. CLIP LONGERON END STA 360 L26R AT FWD COMPARTMENT (C1) WAS REPLACED PER B717-200 SRM 51-41-02-0G AND 51-41-05-0G. (LP #0181288)
- [SDR DALA2024012601170](https://openairdocs.org/sdr/DALA2024012601170.md): Floor Support · cracked · Jan 25, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1). SUMMARY OF NRC 00170: FLOOR CHANNEL STA 655 X=-42 Z=-1 APPROX AT FWD COMPARTMENT (C1) WAS REPAIRED PER B717-200 SRM 51-70-11- 2R PROCEDURE 1 REPAIR 1 PARAGRAPH 4 FIGURE 201. (LP #0171182
- [SDR DALA2024012501108](https://openairdocs.org/sdr/DALA2024012501108.md): Cusp Web · corroded · Jan 25, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON ANGLE CUSP BTW STA Y=168 AND STA Y=200, AND STA X=-60 AT PASSENGER COMPARTMENT (R1 ENTRY). SUMMARY OF NRC 00245: CORROSION LEVEL 2. CUSP ANGLE BTW STA Y=168 AND STA Y=200, AND X=-60 AT PASSENGER COMPARTMENT (R1 ENTRY) WAS REPAIRED PER ERA 614741-1
- [SDR DALA2024012200906](https://openairdocs.org/sdr/DALA2024012200906.md): Angle · cracked · Jan 20, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACK ON ANGLE STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1. SUMMARY OF NRC 00073: ANGLE (INTERCOSTAL) STA Y=186 AND BTW BEAMS #4/5 AT SERVICE DOOR L1 WAS MANUFACTURED AND REPLACED PER DWG 9955763 REV K, B717-200 SRM 51-41-02-0G, AND 51-41-05-0G. (LP #01640
- [SDR DALA2024011900807](https://openairdocs.org/sdr/DALA2024011900807.md): Web · cracked · Jan 18, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CARCK ON WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX. SUMMARY OF NRC 00342: WEB STA Y=715 -X=44 CABIN FLOOR AT CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0161024)
- [SDR DALA2024011800751](https://openairdocs.org/sdr/DALA2024011800751.md): Cusp Web · corroded · Jan 17, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEB LOWER SURFACE BTW STA Y=435 TO Y=465 PAX CABIN. SUMMARY OF NRC 00558: CORROSION LEVEL 2. RH CUSP WEB BTW STA Y=435 TO Y=465 PAX CABIN WAS REPAIRED PER B717 SRM 53-00-55-2R PROCEDURE 4 REPAIR 4. (LP #0159555)
- [SDR DALA2024011600591](https://openairdocs.org/sdr/DALA2024011600591.md): Web · cracked · Jan 16, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKS ON WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX. SUMMARY OF NRC 00346: WEB BTW STA Y=693 TO Y=615, -X=57, CABIN FLOOR AT CPAX WAS REPAIRED PER B717-200 SRM 53-00-55-2R-4 FIG 203. (LP #0156605)
- [SDR DALA2024011500575](https://openairdocs.org/sdr/DALA2024011500575.md): Unknown · unknown · Jan 13, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON RH CUSP WEBS STA 870 TO 889, L-18R CABIN FLOOR AT CPAX. SUMMARY OF NRC 00485: CORROSION LEVEL 2. CUSP WEBS STA 870 TO 889, L-18R CABIN FLOOR WERE REPAIRED PER B717-200 SRM 53-00-55-2R-4. (LP #0153367)
- [SDR DALA2024011200539](https://openairdocs.org/sdr/DALA2024011200539.md): Unknown · unknown · Jan 11, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION OF MEMBRANE WEP ON STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 00247: CORROSION LEVEL 2. MEMBRANE WEP ON STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PAR 4 A
- [SDR DALA2024011200538](https://openairdocs.org/sdr/DALA2024011200538.md): Unknown · unknown · Jan 11, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CORROSION ON MEMBRANE WEB AT STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1). SUMMARY OF NRC 00247: CORROSION LEVEL 2. MEMBRANE WEB AT STA Y=198 AND STA X=-56 AT PASSENGER COMPARTMENT (W1) WAS REPAIRED PER B717-200 SRM 51-70-10-2R PROCEDURE 2 REPAIR 2 PA
- [SDR DALA2024011000451](https://openairdocs.org/sdr/DALA2024011000451.md): Unknown · unknown · Jan 10, 2024 · N997AT · Boeing 717200 · Fuselage Miscellaneous Structure
  > CRACKED WEB AT STA Y=674 -X=44 CABIN FLOOR IN CPAX. SUMMARY OF NRC 00336: CRACK ON WEB STA Y=674 -X=44 CABIN FLOOR IN CPAX WAS REPAIRED PER B717 SRM 53-00-55-2R-4. (LP #0147690)
- [SDR DALA2023120710009](https://openairdocs.org/sdr/DALA2023120710009.md): Unknown · unknown · Dec 6, 2023 · N997AT · Boeing 717200 · Passenger/Crew Doors
  > DENT ON 1L DOOR SKIN. LEFT LOWER CORNER. DENT MEASURES 3" X.5". FOUND DAMAGE TO PRESSURE SEAL MEASURES APPROX 1.5'. ACCOMPLISHED SECTION 1 FERRY FLIGHT PREPERATION IAW ERA 614189-14 REVISION ORIGINAL. CUT OUT DAMAGE AND REMOVED EXISTING FASTNER FOR REPAIR PER
- [SDR DALA2022053103722](https://openairdocs.org/sdr/DALA2022053103722.md): Battery Pack · inoperative · May 27, 2022 · N997AT · Boeing 717200 · Emergency Lighting
  > FOUND THE CENTER OVERWING EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE CENTER OVERWING EMERGENCY LIGHT BATTERY PACK REF B717 AMM 33 -51. OPERATIONAL CHECK WAS NORMAL. (LP #8632816)
- [SDR DALA2022051003228](https://openairdocs.org/sdr/DALA2022051003228.md): Gasper Fan · seized · May 9, 2022 · N997AT · Boeing 717200 · Air Distribution Fan
  > SHIP 9545 - THE FLIGHT CREW DIVERTED THE AIRCRAFT TO JAX DUE TO A STRONG ODOR IN THE COCKPIT AND SMOKE IN THE CABIN AS REPORTED BY THE CABIN CREW. AN EMERGENCY WAS DECLARED WITH ATC AND THE LANDING AT JAX WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE FOUND TH
- [SDR DALA2021121607775](https://openairdocs.org/sdr/DALA2021121607775.md): None · none · Dec 10, 2021 · N997AT · Boeing 717200 · Fuselage Floor Panel
  > AFT CARGO LOWER DOOR JAMB FROM MID DOOR TO FWD END OF JAMB HAS LARGE AREAS OF SURFACE CORROSION.(M) SUMMARY SEE NRC 054-0009 5300-2007/002 00319: CORROSION LEVEL 2. BLENDED OUT CORROSION AND CHECK LIMITS PER B717 SRM 53-00-00-01A. NDT REQUIRED. PERFORMED U/T O
- [SDR DALA2021110406789](https://openairdocs.org/sdr/DALA2021110406789.md): None · none · Nov 2, 2021 · N997AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY FLOOR PATH LIGHTING AT 19D IS MISSSING. MAINTENANCE REPLACED 19D EMERGENCY FLOOR LIGHT STRIP PER B717 AMM 33-50. OPERATIONAL CHECK WAS GOOD. (LP #2004641)
- [SDR DALA2021092805822](https://openairdocs.org/sdr/DALA2021092805822.md): None · none · Sep 25, 2021 · N997AT · Boeing 717200 · Emergency Lighting
  > THE FORWARD ATTENDANT EMERGENCY EXIT SIGN AND THE CEILING PANELS #11 AND #12 EMERGENCY LIGHTS ARE INOPERATIVE. MAINTENACE REPLACED THE EMERGENCY BATTERY PACKS AT LOCATIONS B5-235 AND B5- 231 PER B717 AMM 33-51. OPERATIONAL CHECK IS NORMAL. (LP #8080547)
- [SDR DALA2021082404983](https://openairdocs.org/sdr/DALA2021082404983.md): Battery Pack · inoperative · Aug 21, 2021 · N997AT · Boeing 717200 · Emergency Lighting
  > THE RIGHT AND LEFT AFT OVERWING EXIT LOWER EMERGENCY EXIT LIGHTS ARE INOPERATIVE. IN REFERENCE TO THE B717 AMM 33-51, MAINTENANCE REPLACED THE EXIT LIGHT POWER AND BATTERY. THE OPERATIONAL TEST WAS GOOD. (LP #7807637)
- [SDR DALA2021120907586](https://openairdocs.org/sdr/DALA2021120907586.md): None · none · Apr 27, 2021 · N997AT · Boeing 717200 · Leading Edge Devices
  > LEADING EDGE SLAT TRACK CUTOUT MISSING ON #3 SLAT. FORWARD CUTOUT DOOR TO CDL 57-47-01. PLACARD INSTALLED. MISSING PART NUMBER IN IPC IS NOT EFFECTIVE FOR THIS A/C. PER BOEING CUSTOMER SUPPORT THERE IS AN IPC MISPRINT WHICH WILL BE CORRECTED IN JANUARY OF 2022
- [SDR DALA2021041902263](https://openairdocs.org/sdr/DALA2021041902263.md): Battery Pack · inoperative · Apr 18, 2021 · N997AT · Boeing 717200 · Emergency Lighting
  > THE EMERGENCY EXIT IDENTIFIER LIGHT AT THE FIRST ROW OF SEATS AND THE OVERHEAD EMERGENCY FLOODLIGHT AT THE SERVICE DOOR ARE BOTH INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK BP-259 PER B717 AMM 33-51. OPERATIONAL CHECK WAS GOOD. (LP #7296636)
- [SDR DALA2020121104051](https://openairdocs.org/sdr/DALA2020121104051.md): Skin · cracked · Dec 10, 2020 · N997AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > VERTICAL STAB ZFS 52.267 LT SKIN CRACK INDICATION. MAINTENANCE COMPLIED WITH ALL STEPS OF PRI 588955-14AD REV ORIG, 1, 2, 3, AND 4. COMPLIED WITH TIME LIMITED REPAIR SECTION 1 OR ER/A 588955-14AD REV ORIGINAL.
- [SDR DALA2020121104050](https://openairdocs.org/sdr/DALA2020121104050.md): Spar Cap · cracked · Dec 10, 2020 · N997AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > THE THIRD BOLT HOLE BELOW STA ZFS=52.267 ON LT VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA 5530-01048 AND AD 2018-10-08. MAINTENANCE COMPLIED WITH CRACK VERIFICATION, PER AMDS 5530-01048-02 AND CRACK INDICATION STILL PRESENT. VERIFIED CRACK IN
- [SDR DALA2020121004034](https://openairdocs.org/sdr/DALA2020121004034.md): Spar Cap · cracked · Dec 10, 2020 · N997AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > 4TH BOLT HOLE BELOW STA ZFS=52.267 ON LT SIDE OF VERTICAL STAB FRONT SPAR CAP HAS CRACK INDICATION, REF AA5530-01048 & AD 2018 -10-08. C/W CRACK VERIFICATION, PER AMDS 5530-01048-02 STEP 10. CRACK DETERMINED IN SKIN (QC1432). STEPPED SKIN HOLE TO.277. C/W
- [SDR DALA2022092906387](https://openairdocs.org/sdr/DALA2022092906387.md): None · none · Dec 9, 2020 · N997AT · Boeing 717200 · Vertical Stabilizer, Spar/Rib
  > DAMAGE TOLERANCE EVALUATION ERA 5882955-14AD ISSUED FOR VERTICAL STABILIZER SKIN CRACK REPAIR. FOLLOW ON ACTION REQUIRED. ACCOMPLISH DAMAGE TOLERANCE EVALUATION PRIOR TO 24 MONTHS FROM SECTION I ACCOMPLISHMENT. ERA REVISION REQUIRED FOR A/C OPERATION BEYOND 24
- [SDR DALA2020112303836](https://openairdocs.org/sdr/DALA2020112303836.md): Frame · cracked · Nov 21, 2020 · N997AT · Boeing 717200 · Fuselage Main, Frame
  > A CRACK WAS FOUND ON THE REAR FRAME (48 SECTION UPPER). THE AFT TAIL CONE WAS DROPPED. MAINTENANCE REMOVED THE DAMAGED 48 SECTION OF THE UPPER FRAME AND INSTALLED A NEW 48 SECTION UPPER FRAME, PER BOEING DRAWING 5966768.
- [SDR DALA2020111203697](https://openairdocs.org/sdr/DALA2020111203697.md): Access Door · missing · Nov 10, 2020 · N997AT · Boeing 717200 · Elevator, Plate/Skin
  > DURING THE POST-FLIGHT INSPECTION, THE PILOT DISCOVERED THAT THE RIGHT ELEVATOR OUTBOARD MOST HINGE NUT LOWER ACCESS DOOR WAS MISSING. MAINTENANCE FORWARDED IT TO CDL 55-25-01, DUE TO NOT A STOCK ITEM. NO "M" PROCEDURES. PLACARD WAS INSTALLED. ALSO, PERFO
- [SDR DALA2020102603460](https://openairdocs.org/sdr/DALA2020102603460.md): Skin · cracked · Oct 25, 2020 · N997AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > LT SIDE OF VERTICAL STAB LEADING EDGE HAS 3 CRACK INDICATIONS IN HOLES NR 2, 3, & 4 BELOW STA 2FS=52.267, REF AMDS CARD 5530-01048-02 STP 8, AA5530-01048 AD 2018-10-08. RE-EVALUATION OF FASTENER HOLES FOUND HOLES NR 3 & 4 WITH NO CRACK INDICATION. HOLE NR 2
- [SDR DALA2020102603459](https://openairdocs.org/sdr/DALA2020102603459.md): Skin · cracked · Oct 25, 2020 · N997AT · Boeing 717200 · Vertical Stabilizer, Plate/Skin
  > THE RT SIDE OF VERTICAL STAB LEADING EDGE HAS A CRACK INDICATION IN HOLE NR 3 BELOW STA 2FS=52.267, REF AMDS CARD 5230-01048-02 STEP 8, AA 5530-01048 AD 2018-10-08. INSPECTED RT HORIZONTAL STAB HOLE NR 3. BHEC IAW CARD 5330-01048-02. CRACK INDICATION IS IN
- [SDR DALA2022092906386](https://openairdocs.org/sdr/DALA2022092906386.md): None · none · Oct 24, 2020 · N997AT · Boeing 717200 · Fuselage Structure (General)
  > DAMAGE TOLERANCE EVALUATION IN REFERENCE TO ERA 588282-14AD. ASSOCIATED ER/A 14-588282 ADDED FOR AC 9545. UPDATED MONITOR TITLE. REFER TO ERA 588955-14AD AND MONITOR 1674753 FOR ADJACENT REPAIR WHICH ALSO IS PENDING STAGE II/ III DAMAGE TOLERANCE EVALUATION. N
- [SDR DALA201904222553](https://openairdocs.org/sdr/DALA201904222553.md): Frame · cracked · Apr 19, 2019 · N997AT · Boeing 717200 · Fuselage Main, Frame
  > FUSELAGE FRAME AT STA Y 696 RT SIDE HAS A CRACK. REF AA 5310-01436 CRACK IS CONDITION 3. NRC 026-0004:5310-01436-01D/001 00060: REPLACED FRAME AT STA 696 RH PER WORK CARD 5310-01436-03B. (LP #1037420)
- [SDR DALA201811206696](https://openairdocs.org/sdr/DALA201811206696.md): Slide · unserviceable · Nov 17, 2018 · N997AT · Boeing 717200 · Escape Slide
  > DURING TAIL CONE ESCAPE SLIDE PIN CHECK, MAINTENANCE FOUND THE SLIDE TO BE UNSERVICEABLE (FAULT NOT SPECIFIED). MAINTENANCE REPLACED THE TAIL CONE SLIDE PER B717 AMDS CARD 2561-9006. NO FURTHER DEFECTS NOTED. THE AIRCRAFT HAS RETURNED TO SERVICE. (LP #4427198)
- [SDR DALA2018021400884](https://openairdocs.org/sdr/DALA2018021400884.md): Light · inoperative · Feb 14, 2018 · N997AT · Boeing 717200 · Emergency Lighting
  > RIGHT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT IAW AMM 33-50, OPS CHECKED GOOD.
- [SDR DALA2017061504722](https://openairdocs.org/sdr/DALA2017061504722.md): Doubler · cracked · Jun 14, 2017 · N997AT · Boeing 717200 · Fuselage Main, Plate/Skin
  > CRACK ON PRODUCTION DOUBLER BS 1178 BETWEEN LONGERONS 19R TO 20R. REPAIRED IAW DWG 9911859, REV BU AND SRM 51-20-09.

Next page: https://openairdocs.org/aircraft/N997AT/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N997AT' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N997AT/reports

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